View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 61183U 26145.20873456 +.00000000 +00000-0 +00000-0 0 00005
2 61183 55.1893 221.9512 0002451 218.9460 138.6391 1.70474453 02
| Epoch (UTC): | 25 May 2026 05:00:34 |
| Eccentricity: | 0.0002451 |
| inclination: | 55.1893° |
| perigee height: | 23215 km |
| apogee height: | 23229 km |
| right ascension of ascending node: | 221.9512° |
| argument of perigee: | 218.9460° |
| revolutions per day: | 1.70474453 |
| mean anomaly at epoch: | 138.6391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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